Effects of independent variations of mach number and reynolds number on the maximum lift coefficients of four NACA 6-series airfoil sections
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Effects of independent variations of mach number and reynolds number on the maximum lift coefficients of four NACA 6-series airfoil sections, report, November 1952; (https://digital.library.unt.edu/ark:/67531/metadc56326/: accessed March 29, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.